NADAR SARASWATHI COLLEGE OF ENGINEERING AND TECHNOLOGY Vadapudupatti, Theni-625531 Question Bank for the Units I to V SE05 BR05 SU02 5 th Semester B.E. / B.Tech. Electrical & Electronics engineering IC6501 Control Systems Part-A (10 x 2 = 20 Marks) 1. What is control system? 1. Define transfer function. 1. Distinguish between open loop and closed loop system. 1. Why negative feedback is invariably preferred in closed loop system? 1. What are the components of feedback control system? 2. What is sink and source? 2. Write the analogous electrical elements in force voltage analogy for the elements of mechanical translational system. 2. Write Masons Gain formula. 2. Name two types of electrical analogous for mechanical system. 2. What is servomechanism? 3. What are transient and steady state response? 3. What is an order and type of a system? 3. Define Damping ratio.. 3. List the time domain specifications.
3. Define delay time, rise time, peak time, peak overshoot & settling time 4. Why derivative controller is not used in control systems? 4. What is the type and order of the system? G(s) =K/s (Ts+1) 4. Define Steady state error. 4. What is step, ramp & parabolic signal? 4. What are the three constants associated with a steady state error? 5. What is frequency response? 5. Define resonant Peak and resonant frequency? 5. What is bandwidth and cutoff rate? 5. Define Gain Margin and phase margin. 5. Define Gain cross over and phase cross over. 6. What is Bode plot? 6. What is polar plot? 6. What type of compensator suitable for high frequency noisy environment? 6. What is non-minimum phase transfer function? 6. What is the transfer function of lag/lead compensator? 7. What is feedback compensation? 7. What is lead lag compensation? 7. What are the time domain specifications needed to design a control system? 7. What are the two types of compensation? 7. What are the uses of lag and lead compensator?
8. What are the frequency domain specifications neded to design a control system? 8. What are root loci? 8. Define BIBO stability. 8. What is the necessary condition for stability? 8. What is state variable? 9. What are the properties of state transition matrix. 9. What is state vector? 9. What is controllability? 9. What is observability? 9. List some advantages of phase variable method 10. What is the need for controllability test? 10. What is the need for observability test? 10. Define time invariant system. 10. What are the disadvantages of Transfer function approach? 10. Write the state model of linear time invariant system. Part B ( 5 x 13 = 65 Marks) 11.a. Derive the transfer function for Armature controlled DC motor. (13) 11.a. Determine the transfer function Y(s) /F(s) of the system shown in fig.
11.a. With neat diagram, explain the working of AC servo motors. (13) 11.a. Find the overall gain of the system whose signal flow graph is shown in fig. (13)
11.a. With neat diagram, explain the working of DC servo motors. (13) 11.b. Draw a signal flow graph and evaluate the closed loop transfer function of a system whose block is shown in fig (13) 11.b. Derive the transfer function for field controlled DC motor. (13) 11.b. With neat diagram, explain the working of synchros. (13). 11.b. For the system represented by the block diagram shown in fig. Determine C1/R1 andc2/r1 (13)
11.b. Obtain the closed loop transfer function C(S)/R(S) of the system whose block diagram is shown in (13) fig.
12.a. A unity feedback control system has an amplifier K A =10 and gain ratio, G(s)=1/s(s+2) in the feed (13) forward path.a derivative feedback, H(s)=sK 0 is introduced as a minor loop around G(s).Determine the derivative feedback Constant, K 0 so that the system damping factor is 0.6. 12.a. (i)derive the expressions and draw the response of first order system for unit step i/p. (6) (ii) Draw the response of second order system for critically damped case and when input is unit step. (7) 12.a. Derive the expressions for Rise time, Peak time, Peak overshoot, settling time (13) 12.a. A positional control system with velocity feedback is shown in fig. What is the response of the system (13) for unit step input. 12.a. i) Measurements conducted on a Servomechanism show the system response to be c(t)=1+02.2e-60t-1.2e -10t. (6) When subjected to a unit step. Obtain an expression for closed loop transfer function. ii)a positional control system with velocity feedback is shown in fig. What is the response c(t) to the unit (7) step input. Given that ς =0.5.and also calculate rise time, peaktime, Maximum overshoot and settling time.
12.b. A unity feedback control system has an OLTF, G(s)= K/(s(s 2 +4s+13).Sketch the root locus. (13) 12.b. (i)for a unity feedback control system the open loop transfer functiong(s) = 10(s+2)/s 2 (s+1).find (a) position, velocity and acceleration error constants. (b)the steady state error when the input is R(s) where (6) R(s)=3/s-2/s 2 +1/3s 3 (ii) For a servomechanisms with open loop transfer function 1.G(s)=10/(s+2)(s+3), (7) 2. G(s)= 20(s+2)/s(s+1)(s+3).What type of input signal gives constant steady state error and calculate its value. 12.b. The open loop transfer function of a servo system with unity feedback system is G(s) = 10/ s(0.1s+1). (13) Evaluate the static error constants of the system. Obtain the steady state error of the system when subjected to an input given Polynomial r(t) = a 0 +a 1 t +a 2 /2 t 2. 12.b. The unity feedback system is characterized by an open loop transfer function is G(s) = K / s(s+10). (13) Determine the gain K,so that the system will have a damping ratio of 0.5.For this value of K, determine Settling time, peak overshoot and time to Peak overshoot for a unit-step input. 12.b. A unity feedback control system is characterized by the following open loop transfer function (13) G(s) = (0.4s+1)/s(s+0.6).Determine its transient response for unit step input and sketch the response. Evaluate the maximum overshoot and the corresponding peak time. 13.a. Plot the Bode plot for the following transfer function and obtain the gain and phase crossover frequencies. (13) G(s)=75(1+0.2s)/s(s 2 +16s+100) 13.a. Discuss the correlation between time and frequency response of second order system. (13) 13.a. Consider a unity feedback system having an open loop transfer function,g(s)=k/s(1+0.5s)(1+4s). (13) Sketch the polar plot and determine the value of K so that (i) Gain margin is 20 db and (ii) Phase margin is 30'. 13.a. How does closed loop frequency response is determined from the open loop frequency response (13) using Nichols chart? Explain how the gain adjustment is carried out on the Nichols chart. 13.a. Plot the Bode plot for the following transfer function and obtain the gain and phase crossover frequencies. (13)
G(s)=10/s(1+0.4s)/(1+0.1s) 13.b. For the function, G(s) = 5(1+2s)/(1+4s)(1+0.25s),draw the bode plot. (13) 13.b. The open loop transfer function of a unity gain feedback system is given by G(s) =1/s 2 (1+s)(1+2s). (13) Sketch the polar plot and determine the gain margin and phase margin 13.b. The open loop transfer function of a unity gain feedback system is given by G(s) =1/s(1+s) 2. Sketch the polar plot and determine the gain margin and phase margin (13) 13.b. Consider a unity feedback system having an open loop transfer function, G(s)=K/s(1+0.2s)(1+0.05s). (13) Sketch the polar plot and determine the value of K so that (i) Gain margin is 18 db and (ii) Phase margin is 60'. 13.b. A unity feedback control system has an OLTF, G(s)=K/s(1+2s).Design a suitable lag compensator so that (13) the phase margin is 40 º & the steady state error for ramp input is less than or equal to 0.2 14.a. Describe the procedure for the design of lead compensator using bode plot. (13) 14.a. Describe the procedure for the design of lag compensator using bode plot. (13) 14.a. Describe the procedure for the design of lag compensator using bode plot. (13) 14.a. The open loop transfer function of a unity feedback control system is given by (13) G(S) =K/(S+2) (S+4) (S 2 +6S+25). By applying the routh criterion, discuss the stability of the closed loop system as a function of K. Determine the values of K which will cause sustained oscillations in the closed loop system. What are the corresponding Oscillation frequencies? 14.a. Draw the Nyquist plot for the system whose open loop transfer function isg(s) = K / s(s+2) (s+10). (13) Determine the range of k for which closed loop system is stable.
14.b. Determine the range of K for stability of unity feedback system whose open loop transfer function is (13) G(s) = K / s (s+1)(s+2) 14.b. The open loop transfer function of a unity feed back system is given by G(s) = K (s+1) / s3+as2+2s+1. (13) Determine the value of K & a so that the system oscillates at a frequency of of 2 rad/sec. 14.b. 14.b. Construct Routh array and determine the stability of the system represented by the characteristics equation S 5 +S 4 +2S 3 +2S 2 +3S+5=0.Comment on the location of the roots of characteristic equation (13) Construct Routh array and determine the stability of the system represented by the characteristics equation S 7 +9S 6 +24S 4 +24S 3 +24S 2 +23S+15=Comment on the location of of the roots characteristic equation (13) 14.b. Design suitable lead compensators for a system unity feedback and having open loop transfer function (13) G(s)= K/ s(s+1) to meet the specifications.(i) The phase margin of the system 45º,(ii) Steady state error for a unit ramp input 1/15, (iii) The gain cross over frequency of the system must be less than 7.5 rad/sec. 15.a. Write the state equation for a mechanical system shown in fig (13) 15.a. For the given circuit shown in fig. Obtain the State equations the input voltage source is u(t) and the output y(t) is taken across capacitor c 2 (13)
15.a. Obtain and briefly explain the state space representation of Field controlled dc motor. (13) 15.a. Determine the canonical state model of the system, whose transfer function is T(s)=10(s+4)/s(s+1)(s+3). (13). 15.a. Obtain the state model of the system whose transfer function is given by Y(s)/U(s)=10/(s 3 +4s 2 +2s+1) (13) 15.b. Obtain and briefly explain the state space representation of armature controlled dc motor. 15.b. Determine the canonical state model of the system, whose TF is T(s)=2(S+5)/(S+2)(S+3)(S+4) (13) 15.b. Obtain the state transition matrix for the state model whose system matrix A is given by (13) A = 15.b. Check the controllability of the following state space system. (13) x1 º = x 3 x2 º = -2x 1-3x 2 +2u x3 º = 2x 2-3x 3 15.b. Check the observability of the following state space system. (13) x 1 º =x 3
x 2 º = -2x 1-3x 2 +2u x 3 º = 2x 2-3x 3 y= x 1 Part C ( 1 x 15 = 15 Marks) 16.a. Determine the overall transfer function C(S)/R(S) for the system shown in fig (15) 16.a. Sketch the root locus of the system whose open loop transfer function is G(s)=K/s(s+2)(s+4).Find the (15) value of K so that the damping ratio of the closed loop system is 0.5. 16.a. 16.a. Sketch the Bode plot for the following transfer function and determine the system gain K for the gain cross over frequency to be 5 rad/sec. G(s)= Ks 2 /(1+0.2s)(1+0.02s). (15) Design suitable lead compensators for a system unity feedback and having open loop transfer function G(s)= K/ s(s+1)(s+5) to meet the specifications.(i) Velocity error constant Kv 50,(ii)Phase margin 20 º (15) 16.a. A feedback system has a CLTF Y(s)/U(s)=10(s+2)/(s)(s+1)(s+4).Construct three different models for this system and give block diagram representation for each state model. (15) 16.b. Find the overall gain C(s) / R(s) for the signal flow graph shown below. (15)
. 16.b. A unity feedback control system has an OLTF, G(s)=K(s+9)/s(s 2 +4s+11).Sketch the root locus. (15) 16.b. Consider a unity feedback system having an open loop transfer function, G(s)=(1+0.2s)(1+0.025s)/s 3 (1+0.005s)(1+0.001s). (15) Sketch the polar plot and determine Gain and Phase margin. 16.b. Design suitable lead compensators for a system unity feedback and having open loop transfer function (15) G(s)= K/ s(s+8) to meet the specifications.(i) Velocity error constant Kv 10,(ii)Percentage peak overshoot=9.5% (iii)natural frequency of oscillation, wn= 12 rad/sec. 16.b. Construct a state model for a system characterized by the differential equation, (15) d 3 y/dt 3 +6d 2 y/dt 2 +11dy/dt+6y+u=0.Give the block diagram representation of the state model.